Flying-machine.



I. BKRGZ (NOW BY JUDICIAL CHANGE OF NAME I. BETRGZ. FLYING MACHINE.

nruouxou mum DEO.18,1911.

1 7 655 Patented Sept. 23,1913.

2 BHEETEVSHEET 1.

l 2.3 2 J9 3 go i a; 35 x a, 1 5 5 4* M J m J. BARUZ (NOW BY JUDICIAL CHANGE OF NAME J. BEiRGZ).

FLYING MACHINE.

APPLIUATION FILED DEC 16, 1911.

2 SHEETS-43113211 2.

formerly Patented Sept. 23, 1913.

i ihiiiiii Yb (1/! iii/HM if may mmwm:

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hiy 'iimruii m ml hi iijyilli f and it com: :5 iiiwitiy Lhii IH'HVi 'jmimhie ghaiiiig wings. iittmi whzh ii; ii Wings i iiiich iaiitm' have sh iiri iHlW-Whui" ion.

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i i. '1 sis is ohiizihhii h having on the i hi'iiii' whiinh is; ii if, imiumcimi with the am tiu ihii *i 1M 5 iii th n wi w' i, ii two-sinned kiwi wmi which urn: rods 10 pmiw t0 hi3 i hi'i zlciii 153 iimri h) the g iiiriiir g h 1 mi ihii iiiiiiiii'ih of the turning pm i? iiih ["Qlii; i0, ihii short ii'in g 9 Wiii hi: i" ,iiii iii hike the pmailiiii hmvn by doihm him in i iiiiiii, ei, 'ihm'niiom, with m m i I H! ihh ii'iflj g ii reduced imp iii ui i.

Viol hi the iiyiiljlj 131mm are organism vi'hiiiehy the rudliiii hiiihihlc 50 ms to inure: f!i!lLi'y -1f-Phipfl iij", whih: u Lilo same time Eh Milfh ni'iri: @I'Uliliii is; facilitated by Miami: this (h'mvin; ;;-i11 of the rudder. i iii this: iiiirpoiiu, {he steering shaft propiel' ii is: i'i nilfliiil in ii huliuw shaft 1 1 and ML ihhri-iii h :avi screws '15. The iiihiii iii ih; imrii'urd end 'iii'iti hm?! with :i steering 1e- [mum ifili, imiiuw :ihufi 1'1 Wiiil the whoring shsiji'i" i :U'Hi ihu imhhw' 20. This rvduving hi himii'ryih (fliikil'iihY hf tho rudder will iuitiiz'iiiiv minim ihu ii-imw n1- i-ziihei' the rud- (ili' iii iii iQM'PI'PLii fiiimuiinnvnusly with the 'imvvi-ing'g iii? ihu rmhh-i', have occurs 1L hit- (mi riiiiplhcvimmi (if Hi0 lying machine 111 that ihi iwie; iiiliYLilJii is iivfh-uted from its n "viuus; mm'sv. The imvvrii g of the rud- (iPi' hiw'w'ii ih'ia mm 01" he 01 hm. Silili is shmvn iii Hm i f; hhii h,

in (lilill' in um: ihi'i rudder for vertical .-1i1&liil 1,f iii riifij iriiml by mums of a level 21 whiuh is; cumin-char] with thicsvo 'iing rods 3:2 (inhlifuiiingz: :1 iwmiii'ii'icil lever 23 which ground.

transmits its movements byrods 2% to tie i rudder 20. The rods as also the steering shaft are suitably adjusted endwiseancl then secured by set screws or otherwise so as to avoid unintentional telescoping of same.

At the lower flying frame there are four chain pulleys 28 which carry the seat 27 for the pilot and passengers, the arrangement being such as to insure balancing with vary ing loads. The car can also be connected. with the lever 21 so that the rudder 20 shall be automatically regulated under great toss vantageously be suspended from the middle cross bar 29 of the flying frame. It is to be remarked that the car must be rigidly fixed to the frame during the transport over This can be effected by means of a nut on the pivot bolt 30 whereby the car can be held ripidly in position. This is nec;

essary because the car is fitted with the third runner wheel 31 which latter may be used. for steering by means of the hand-Wheel T he Wings 4 receive movement from the motor through the intervention of rods 33 of eccentrics, and which rods are attached to a block 34.- moving in a slotted guide 35 and operziting connecting rods 36 With cranks 37. The crank-shaft 38 is mounted in bearings 39 fixed to the flying frame 1. The crank-shaft is connected with the shaft 40 ofothc flapping Wings l by means of uni- .ersal joints 41 so that said Wings can be operated in any position of'the gliding wings or planes 2. The flying frame is com.- posed of tubes which serve as reservoirs for liquid fuel for the motor.

It may be remarked that the driving mechanism, when the flight is in the direction of the wind, can be temporarily uncoupled and that only at more or less long intervals a few strokes of the flapping Wing's may be carried out. For this purpose the driving mechanism is fitted with any suitable friction clutch one part of which is fast on the motor shaft.

Before using the flying machine it will naturally be necessary to properly adjust? and iii; the telescoping and collapsible parts) of the machine.

What I claim as my invention and to secure by l ictters Patent is:

L A flying machine, comprising a frame, adjustably disposed gliding Wings, flapping .wings, attached to the latter movable flaps in the frame of said flapping Wings and automatically turn-over surfaces at the outer side of the frame of said flapping Wings said flaps of the lapping Wings being closed at three sides, substantially as set forth.

2. A flying machine, comprising a frame, adjustably disposedglidinp; Wings, flappine Wings attached to the latter movable flaps in the frame of said flapping Wings and an tomatically turn'over surfaces at the outer ing of the flying machine. the car may ad desire adjustably disposed side of the frame of said flapping wings said articulated surfaces being turned over by means of a two-armed lever fast on the axis of said surfaces and having theends pivotally connected with crossed rocs the other ends of which rods are held. in sta 'l'iouary positions, substantially as set forth.

A flying; machine, comprising a frame, adjustabiy disposed gliding wings, flapping wings, attached to the latter, the shaft of said flapping Wings being journaled on said gliding Wings and arranged at an. acute angle With the longitudinal axis of said if ing' frame, movable flaps in the rame of said flapping Wings and automatically turnover surfaces at the outer side of the frame of said flapping Wing's, said flaps of the flapping wings being closed at three sides, substantially as set for h.

4. A flying machine, comprising a frame, adjustably disposed gliding wings, flapping wings, attached to the latter, the shaft of said flapping Wings being journaled on said gliding Wings and arranged at an acute angle with the longitudinal axis of said ing fram movable flaps in the frame of said flapping Whigs and automatically turnover surfaces at the outer side of the frame of said flapping ings, said flaps of the flapping s ings being closed at three sides, a motor arranged in said frame, a crank operated by said motor, and a universal joint for connecting said crank to said shaft of said flapping Wings, substantially as set forth.

5. It flying machine, comprising a frame, adj'ustably disposed gliding Wings, flapping Wings, attached to the latter, the shaft of said flapping Wings being jouriialed on said gliding wings and arranged at an acute angle with the longitudinal axisaof said flying frame, movable flaps in the frame of said flapping win s and automatically turnover surfaces at the outer side of the frame of said flapping Wings, said flaps of the flapping lvings being closed at three sides and a steering shaft turnable in said frame,

a rudder connected Wltll said steering shaft and turnable on its transverse middle axis, and a lever comicctiou for turning said rudder on its transverse middle axis, substantially as set forth.

6. A flying machine, comprising a frame, gliding wings, flapping wings, attached to the latter, the shaft of said, flapping wings being journaled on said gliding wings and arranged. at an acute angle with the longitudinal axis of said flying frame, movable flaps in the frame of said flapping .vings and automatically turn over surfaces at the outer side of the frame of said flapping wings, said flaps of the flapping Wu J steering shaft turnable in said frame, a rudder connected with said steering shaft and s being closed at three sides, a-

turnable on its transverse middle axis, and 1911, in the presence of two subscribing witrods for turning sald rudder on its transnesses.

verse middle axis said steering shaft and said rods being C OIHPOSECi of several tele- JOSEF BARGZ' 5 scoping parts, substantially as set forth. W'itnesses:

In testimony whereof I have hereunto Loms VANDORY,

signed my ame this 1st day of December THERESA THRONBERENA. 

